# Service difficulty reports: N961AT

A list on [N961AT](https://openairdocs.org/aircraft/N961AT.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 198 reports

- [SDR DALA2026101305626](https://openairdocs.org/sdr/DALA2026101305626.md): Skin · dented · Oct 10, 2026 · N961AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUR DENTS IDENTIFIED COMMON TO AFT INSTALLATION DOUBLER BETWEEN L2R AND L3R FRAME Y541 TO Y560. REPAIRED PER ER/A 637249-14. (1858631) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100805561](https://openairdocs.org/sdr/DALA2026100805561.md): Skin · demodification · Oct 7, 2026 · N961AT · Boeing 717200 · Standard Practices/Structures
  > FOUND EXISTING (DEMOD) ANTENNA, INCLUDING AN INTERNAL DOUBLER, INTERFERING WITH STC DOUBLER BETWEEN Y503 TO Y522 AND STRG L-1 TO STRG L-3R, COMPLIED WITH ER/A 637253-14. (1853917) (AIRCRAFT GROUNDED).
- [SDR DALA2026070303900](https://openairdocs.org/sdr/DALA2026070303900.md): Light · inoperative · Jul 3, 2026 · N961AT · Boeing 717200 · Emergency Lighting
  > LEFT OVERWING EMERGENCY EVACUATION LIGHT INOPERATIVE. REPLACED LIGHT IAW AIPC 33-50. (8777078) (AICRAFT GROUNDED).
- [SDR DALA2025102207715](https://openairdocs.org/sdr/DALA2025102207715.md): Cable · twisted · Oct 20, 2025 · N961AT · Boeing 717200 · Aerodynamic Fairings
  > SHIP 9520 DURING SSE WAS FOUND TWISTED PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT. CORRECTIVE ACTION: PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT WAS INSTALLED CORRECTLY PER B717-200 AMM 53-52-01-830-802 ONL
- [SDR DALA2025102207714](https://openairdocs.org/sdr/DALA2025102207714.md): Cable · twisted · Oct 20, 2025 · N961AT · Boeing 717200 · Aerodynamic Fairings
  > DURING SSE WAS FOUND TWISTED PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT. PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT WAS INSTALLED CORRECTLY PER AMM 53-52-01-830-802 ONLY STEP E. (1) (S). (1262180)
- [SDR DALA2025102207716](https://openairdocs.org/sdr/DALA2025102207716.md): Door Frame · cracked · Oct 18, 2025 · N961AT · Boeing 717200 · Fuselage Main, Structure
  > SHIP 9520 CRACK OF 0.350IN LENGTH WAS FOUND ON LH OVERWING FRAME STA Y=737 IN REFRENECE TO CARD 5310-01439-01B / JOB 068-0003, STEP 4. LEFT OVERWING FRAME STA Y=737 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (1258141)
- [SDR DALA2025102207713](https://openairdocs.org/sdr/DALA2025102207713.md): Seal · leaking · Oct 18, 2025 · N961AT · Boeing 717200 · Emergency Exits
  > DURING STATIC LEAK CHECK, WATER LEAKS WERE FOUND ON INSIDE OF FWD AND AFT LT OVERWING EMERGENCY EXIT DOORS. EXIT DOOR JAMB FILLER FWD AND AFT LT WERE REPLACED PER AMM 53-12-01 AND STATIC LEAK CHECK WAS PERFORMED PER AMM 52-21-01-790-801 AND NOT LEAKS WERE FO
- [SDR DALA2025102207712](https://openairdocs.org/sdr/DALA2025102207712.md): Fuel Tank · corroded · Oct 18, 2025 · N961AT · Boeing 717200 · Fuel Storage
  > EXFOLIATION ON LOWER SKIN OF CENTER FUEL TANK ON STA Y= 756 AND X= 43 AT LEFT MLG WHEEL WELL. LEFT MLG WHEEL WELL WAS REPAIRED PER ER/A 629799-14AD REV. (1258160)
- [SDR DALA2025102207711](https://openairdocs.org/sdr/DALA2025102207711.md): Release Mech · out of position · Oct 17, 2025 · N961AT · Boeing 717200 · Aerodynamic Fairings
  > IN REFERENCE AMDS 5352-4002 DURING INSTALL TAILCONE SLIDE WAS FOUND TAILCONE RELEASE MECHANIS CAM OUT POSITION. TAILCONE RELEASE MECHANISM CAM WAS ADJUSTED PER AMM 53-52-03 (1257600)
- [SDR DALA2025101707592](https://openairdocs.org/sdr/DALA2025101707592.md): None · none · Oct 10, 2025 · N961AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9520 DTA ER/A 629799-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 10-OCT-25. CORRECTIVE ACTION: REPAIRED PER DTA ER/A 629799-14 (1250137)
- [SDR DALA2025041102826](https://openairdocs.org/sdr/DALA2025041102826.md): Battery Pack · inoperative · Apr 10, 2025 · N961AT · Boeing 717200 · Emergency Lighting
  > IN THE AFT TAIL SECTION, ALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND A BAD BATTERY PACK. THE BATTERY PACK WAS REPLACED IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. LOCATION B5-260. (LP #7244582)
- [SDR DALA2025041102825](https://openairdocs.org/sdr/DALA2025041102825.md): Sign · inoperative · Apr 10, 2025 · N961AT · Boeing 717200 · Emergency Lighting
  > EXIT SIGN ABOVE AFT TAIL DOOR INOPERATIVE. MAINTENANCE REMOVED THE SIGN ASSEMBLY, FOUND WIRES DISCONNECTED, SECURED WIRES, AND THE LIGHT NOW OPERATIONALLY CHECKS GOOD IAW B717 AMM 33-51. (LP #7244583)
- [SDR DALA2025040802707](https://openairdocs.org/sdr/DALA2025040802707.md): Cable · broken · Mar 27, 2025 · N961AT · Boeing 717200 · Emergency Equipment
  > THE FLIGHT ATTENDANT FOUND THAT THE FRONT SERVICE DOOR EMERGENCY CABLE TO BAR WAS BROKEN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE INSTALLED A NEW 1R DOOR SLIDE LATCH/LANYARD A
- [SDR DALA2025031401971](https://openairdocs.org/sdr/DALA2025031401971.md): Skin · gouged · Mar 12, 2025 · N961AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > BANANA FAIRING ATTACH SCREWS HAVE GOUGED INTO THE L/H STABILIZER SKIN PANEL. MAINTENANCE REPLACED LH VERT STAB SKIN TIP PER B717 SRM 51-40. (LP #6408784)
- [SDR DALA2025010300047](https://openairdocs.org/sdr/DALA2025010300047.md): Battery Pack · inoperative · Jan 1, 2025 · N961AT · Boeing 717200 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS FROM ROW 15 TO 19 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK FOR CORRESPONDING LIGHTS PER B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. OK FOR SERVICE. (LP #6601810)
- [SDR DALA2025011500349](https://openairdocs.org/sdr/DALA2025011500349.md): Door · missing · Dec 15, 2024 · N961AT · Boeing 717200 · Accessory Compartment Doors
  > EXTERNAL POWER RECEPTACLE DOOR MISSING. FWD TO CDL 52-47-01 ON 15DEC24 IN LEX. FLIGHT CREW PLACARD INSTALLED. ON 14JAN25 MAINTENANCE INSTALLED A NEW DOOR ASSY PER B717 AMM 24-24. OPERATIONAL CHECK WAS GOOD. CDL & PLACARDS REMOVED. (LP #0711663)
- [SDR DALA2024111410953](https://openairdocs.org/sdr/DALA2024111410953.md): Doubler · cracked · Nov 8, 2024 · N961AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > -AD- FUSELAGE PLATE SKIN DOUBLERS STA Y=1178 BTW L1-L3 LH CRACKED. ACCOMPLISH ER/A 546495-14AD REV A SECTION III FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-546495 ADD
- [SDR DALA2024083008601](https://openairdocs.org/sdr/DALA2024083008601.md): Sign · inoperative · Aug 29, 2024 · N961AT · Boeing 717200 · Emergency Lighting
  > FOUND L/H AND R/H OVERWING EXIT DOOR SIDE PANEL IDENTIFIER SIGN INOPERATIVE. CONFIRMED NO POWER AT PIN 1 OF EITHER EEI. VERIFIED GOOD GROUND. POWER SUPPLY B5-118 TO EEI SIGNS (L2-834 AND L2-835). FOUND FUSES F3 AND F4 BLOWN IN POWER SUPPLY. REPLACED POWER SUPP
- [SDR DALA2024021301998](https://openairdocs.org/sdr/DALA2024021301998.md): Power Supply · inoperative · Feb 13, 2024 · N961AT · Boeing 717200 · Emergency Lighting
  > THE FORWARD OVERWING LOWER EXIT EMERGENCY LIGHTS ON THE LEFT AND RIGHT SIDES ARE INOPERATIVE. MAINTENANCE REPLACED B5-118 BATTERY EMERGENCY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK IS NOW NORMAL AND ALL PANELS ARE CLOSED. (LP #5003415)
- [SDR DALA2023121310202](https://openairdocs.org/sdr/DALA2023121310202.md): Unknown · unknown · Dec 12, 2023 · N961AT · Boeing 717200 · Emergency Lighting
  > BOTH EXTERIOR OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4996665)
- [SDR DALA2023121310201](https://openairdocs.org/sdr/DALA2023121310201.md): Unknown · unknown · Dec 12, 2023 · N961AT · Boeing 717200 · Emergency Lighting
  > BOTH OF THE FWD EMERGENCY DOOR FLOOR IDENTIFIER LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 341 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4996664)
- [SDR DALA2023120409905](https://openairdocs.org/sdr/DALA2023120409905.md): Unknown · unknown · Dec 2, 2023 · N961AT · Boeing 717200 · Emergency Lighting
  > THE EXIT SIGN IS MISSING OVER DOOR 1L. MAINTENANCE INSTALLED A NEW EXIT LIGHT COVER PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4996630)
- [SDR DALA2023102608797](https://openairdocs.org/sdr/DALA2023102608797.md): Unknown · unknown · Oct 25, 2023 · N961AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS REMAIN ON WHILE IN THE "ARM" POSITION. T/S PER B717 FIM 33-50 AND WDM 33-51, PG 2. L2-788, L2-789, AND L2-740 WERE ON IN FLIGHT. ISOLATED AND REPLACED BATTERY AND POWER SUPPLY ASSEMBLY B5-123, PER B717 AMM 33-51. ALL OPERATIONS ARE NOW NOR
- [SDR DALA2023102408721](https://openairdocs.org/sdr/DALA2023102408721.md): Unknown · unknown · Oct 23, 2023 · N961AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS OVER 1L AND 1R DOORS CAME ON IN FLIGHT AND WERE FLICKERING AT A FAST FREQUENCY. CEILING LIGHT OUTSIDE FIRST CLASS LAV ALSO FLICKERED ALONG WITH THE EMERGENCY DOOR LIGHTS. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK B5-259 PER B7
- [SDR DALA2023102408720](https://openairdocs.org/sdr/DALA2023102408720.md): Unknown · unknown · Oct 23, 2023 · N961AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHTS OVER L1 AND L2 DOORS STAY ILLUMINATED. ALL OTHER EMERGENCY LIGHTS OPERATE NORMALLY. *** CONTRACT MAINTENANCE EVENT - OCM: 271512 *** DISCONNECTED AND RECONNECTED THE BATTERY POWER SUPPLY TO L1 AND L2 DOORS EMERGENCY EXIT LIGHTS PER B717 AMM 33
- [SDR DALA2023102308706](https://openairdocs.org/sdr/DALA2023102308706.md): Unknown · unknown · Oct 21, 2023 · N961AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS WERE FLICKERING AT THE L1 DOOR, COCKPIT OVERHEAD, AND OVERHEAD PANEL IN THE CABIN DURING FLIGHT. MAINTENANCE INSPECTED BATTERY PACK B5-123 AND B5-235 PER B717 WD 33-51-12. FOUND BATTERY PACK B5-235 WITH THE BATTERY CONNECTOR BROKEN. REPLAC
- [SDR DALA2023101808566](https://openairdocs.org/sdr/DALA2023101808566.md): Unknown · unknown · Oct 17, 2023 · N961AT · Boeing 717200 · Emergency Lighting
  > DURING THE SERVICE CHECK, MAINTENANCE FOUND BOTH EMERGENCY EXIT LIGHTS IN THE FWD GALLEY INOPERATIVE. SLAVED IN A NEW BATTERY CHARGER UNIT FOR BOTH, AND BOTH LIGHTS FUNCTIONED NORMALLY. MAINTENANCE REPLACED THE BATTERY CHARGER UNIT (B5-118) REF B717 AMM 33-51.
- [SDR DALA2023101608458](https://openairdocs.org/sdr/DALA2023101608458.md): Unknown · unknown · Oct 15, 2023 · N961AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS AT THE TAIL EXIT DOOR AND FORWARD OVERWING EXIT ARE INOPERATIVE. A TERMINAL LUG WAS RE-CONNECTED CORRECTLY AND BATTERY PACKS (B5-235) AND (B5-118) WERE REPLACED PER B717 AMM 33-51-04. TEST OK. (LP #6535998)
- [SDR DALA2023101408443](https://openairdocs.org/sdr/DALA2023101408443.md): Unknown · unknown · Oct 13, 2023 · N961AT · Boeing 717200 · Cargo/Baggage Doors
  > WEAR ON INNER SKIN NEAR TO AFT HINGE, ALSO NEAR TO FWD LATCH FITTING, AT AFT CARGO DOOR. SUMMARY OF NRC 00446: INNER SKIN NEAR TO AFT HINGE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 612398-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 612398-14
- [SDR DALA2023101408441](https://openairdocs.org/sdr/DALA2023101408441.md): Unknown · unknown · Oct 12, 2023 · N961AT · Boeing 717200 · Aerodynamic Fairings
  > A MISSING CLAMP WAS FOUND ON THE LATCH CABLE (2 EA) FOR THE TAILCONE ASSEMBLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00700: LATCH CABLE CLAMPS (2 EA) WERE INSTALLED, LUBE AND
- [SDR DALA2023101408438](https://openairdocs.org/sdr/DALA2023101408438.md): Unknown · unknown · Oct 11, 2023 · N961AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00570: INNER PAN ON STOP #3 AFT EDGE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 612182-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 612182-14 REV. 1. ASSOCIATED ER/A 14-612182 ADDED FOR AC 952
- [SDR DALA2023101408437](https://openairdocs.org/sdr/DALA2023101408437.md): Unknown · unknown · Oct 11, 2023 · N961AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL PRODUCTION DOUBLER BTW EXTERNAL SKIN AND LOWER PAN, AT AFT CARGO COMPARTMENT LOWER DOOR JAMB. SUMMARY OF NRC 0285: CORROSION LEVEL 2. INTERNAL PRODUCTION DOUBLER BTW EXTERNAL SKIN AND LOWER PAN, AT AFT CARGO COMPARTMENT LOWER DOOR JAMB WA
- [SDR DALA2023100608225](https://openairdocs.org/sdr/DALA2023100608225.md): Unknown · unknown · Oct 5, 2023 · N961AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERONS 30, 29L BTW STA 966 TO STA 1002. SUMMARY OF NRC 00565: CORROSION LEVEL 2. CORROSION ON LONGERONS 30, 29L BTW STA 966 TO STA 1002 WERE REPAIRED PER SRM 53-20-05-2R REPAIR 1 FIG 201 (SHEET 1). (LP #0003346)
- [SDR DALA2023100608222](https://openairdocs.org/sdr/DALA2023100608222.md): Unknown · unknown · Oct 5, 2023 · N961AT · Boeing 717200 · Fuselage Main, Structure
  > SEVERAL CORROSION AROUND OF AFT CARGO DOOR JAMB. SUMMARY OF NRC 0007: CORROSION LEVEL 2. AFT CARGO DOOR JAMB WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7 PAR 5 FIGURE 201. (LP #0002390)
- [SDR DALA2023100408151](https://openairdocs.org/sdr/DALA2023100408151.md): Unknown · unknown · Sep 29, 2023 · N961AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION REMOVAL RESULTED IN THE FRAME THICKNESS AT STA Y=275 LONG 30 TO BE OUT OF LIMITS. FWD CARGO. SUMMARY OF NRC 00543: CORROSION LEVEL 2. FRAME AT STA Y=275 LONG 30 FWD CARGO WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3, REPAIR 3. (LP #2993220)
- [SDR DALA2023100308086](https://openairdocs.org/sdr/DALA2023100308086.md): Unknown · unknown · Sep 29, 2023 · N961AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON CAP STA Y=1022RH LONGERON 7RH (INNER STRUCTURE) AT CPAX. SUMMARY OF NRC 00386: CAP STA Y=1022RH LONGERON 7RH INNER STRUCTURE WAS REPAIRED PER ER/A 611872-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-611872 ADDED FOR AC 9520. (LP #299
- [SDR DALA2023100308084](https://openairdocs.org/sdr/DALA2023100308084.md): Unknown · unknown · Sep 29, 2023 · N961AT · Boeing 717200 · Fuselage Structure (General)
  > CORROSION ON CUSP WEB STA Y=965 X=-56 AT CPAX. SUMMARY OF NRC 00669: CORROSION LEVEL 2. CUSP WEB STA Y=965 X=-56 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #2993211)
- [SDR DALA2023092908003](https://openairdocs.org/sdr/DALA2023092908003.md): Unknown · unknown · Sep 28, 2023 · N961AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN BTW STA Y=1076 AND LONGERON 14L. SUMMARY OF NRC 00036: CRACK ON FUSELAGE SKIN BTW STA Y=1076 AND LONGERON 14L.WAS REPAIRED PER PRI 611843-14 REV 2 AND ERA 611843-14 REV ORIGINAL. SECTION I PERMANENT REPAIR.TIME COTROLLED ITEMS: SEC II CO
- [SDR DALA2023092908000](https://openairdocs.org/sdr/DALA2023092908000.md): Unknown · unknown · Sep 28, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB STA Y=370 X=-54 AT CPAX. SUMMARY OF NRC 00668: LEVEL CORROSION 2. CUSP WEB STA Y=370 X=-54 AT CPAX WAS REPAIRED PER B717 SRM-53-00-55-2R PROCEDURE 4 AND 51-41-05-0G PAR 8. (LP #2991582)
- [SDR DALA2023092907999](https://openairdocs.org/sdr/DALA2023092907999.md): Unknown · unknown · Sep 28, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS (2 EA) ON PAN (AFT EDGE) BTW STOP #2 AND #4 OF AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00445: PAN (AFT EDGE) BTW STOP #2 AND #4 OF AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 6 REPAIR 6. (LP #2990723)
- [SDR DALA2023092707959](https://openairdocs.org/sdr/DALA2023092707959.md): Unknown · unknown · Sep 27, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON REPAIR DOUBLERS BTW STA Y=991 / 998, BTW STA Y=743 / 751, AND BTW STA X=54 / 60 AT LH WEBS (PAX CABIN). SUMMARY OF NRC 00405: CORROSION LEVEL 2. DOUBLERS BTW STA Y=991 / 998, BTW STA Y=743 / 751, AND BTW STA X=54 / 60 AT LH WEBS WERE REPLACED PER
- [SDR DALA2023092707957](https://openairdocs.org/sdr/DALA2023092707957.md): Unknown · unknown · Sep 27, 2023 · N961AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME BOTH SIDES, STA 908 BTW L-28R TO L-28L BILGE AREA AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00103: CORROSION LEVEL 2. FRAME BOTH SIDES, STA 908 BTW L-28R TO L-28L BILGE AREA AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G P
- [SDR DALA2023092507866](https://openairdocs.org/sdr/DALA2023092507866.md): Unknown · unknown · Sep 24, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB STA Y=200 TO 218 BTW X=-42 TO X=-54 SIDE RH AT CPAX. SUMMARY OF NRC 00311: CORROSION LEVEL 2. WEB STA Y=200 TO 218 BTW X=-42 TO X=-54 SIDE RH AT CPAX WAS REPLACED PER B717-200 SRM 53-10-51-0I PROCEDURE 2 ITEM 32 AND DWG: 9936535 REV CS. (LP #2
- [SDR DALA2023092507862](https://openairdocs.org/sdr/DALA2023092507862.md): Unknown · unknown · Sep 23, 2023 · N961AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON GENERATION FLOOR PANEL FLOOR PANELS WERE FABRICATED AND REPLACED PER DWG 9952521 REV BB, DWG 9956320 REV G, DWG 9956336 REV G AND B717-200 SRM 51-20-05-0G. (LP #2984188)
- [SDR DALA2023092507858](https://openairdocs.org/sdr/DALA2023092507858.md): Unknown · unknown · Sep 23, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB DOUBLERS (5 EA) RH SIDE; (4 EA) BTW STA Y=503 AND STA Y=579 ON X=-56 AND (1 EA) BTW STA Y=794 AND STA Y=813 ON X=-56 AT PAX CABIN. SUMMARY OF NRC 00323: CORROSION LEVEL 2. CUSP WEB DOUBLERS (5 EA) RH SIDE; (4 EA) BTW STA Y=503 AND STA Y=5
- [SDR DALA2023092007727](https://openairdocs.org/sdr/DALA2023092007727.md): Unknown · unknown · Sep 19, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB STA Y=200 BTW X=0 TO X=12 AT CPAX. SUMMARY OF NRC 00310: CORROSION LEVEL 2. WEB STA Y=200 BTW X=0 TO X=12 AT CPAX WAS REPAIRED PER B717-200 SRM-53-00-00-2R. PROCEDURE 2. (LP #2978093)
- [SDR DALA2023092007726](https://openairdocs.org/sdr/DALA2023092007726.md): Unknown · unknown · Sep 19, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB STA Y=200 BTW X=0 TO X=12 AT CPAX. SUMMARY OF NRC 00310: CORROSION LEVEL 2. WEB STA Y=200 BTW X=0 TO X=12 WAS REPAIRED PER B717-200 SRM-53-00-00-2R. PROCEDURE 2. (LP #2978089)
- [SDR DALA2023092007725](https://openairdocs.org/sdr/DALA2023092007725.md): Unknown · unknown · Sep 19, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB BTW STA Y=579 AND STA Y=598 ON X=-44 (INTERNAL SIDE) AT PAX CABIN. SUMMARY OF NRC 00329: CUSP WEB BTW STA Y=579 AND STA Y=598 ON X=-44 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #2978082)
- [SDR DALA2023091907685](https://openairdocs.org/sdr/DALA2023091907685.md): Unknown · unknown · Sep 18, 2023 · N961AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 6RH STA Y=1022RH (INNER STRUCTURE) AT CPAX. SUMMARY OF NRC 00385: LONGERON ON 6RH STA Y=1022RH (INNER STRUCTURE) AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2. (LP #2976393)
- [SDR DALA2023091907689](https://openairdocs.org/sdr/DALA2023091907689.md): Unknown · unknown · Sep 17, 2023 · N961AT · Boeing 717200 · Escape Slide
  > MISSING RELEASE CABLE AND CLIP RETAINERS (2 EA) ON TAILCONE SLIDE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00130: NEW DEPLOYMENT CABLE WAS INSTALLED PER B717-200 AMM 25-61-02 4

Next page: https://openairdocs.org/aircraft/N961AT/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N961AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N961AT/reports

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